Disengage device for aircraft control

Details Disengage device for aircraft control Disengage device for aircraft control

2008-01-08

2008-01-08

Collins, Timothy D. (Department: 3643)

Aeronautics and astronautics

Aircraft control

Pilot operated

C244S099200

Reexamination Certificate

active

07316373

ABSTRACT:
A disengage device in an aircraft, which prevents a driving force of a drive unit from transmitting to a control surface, having:a first rod having one end portion connected to the drive unit, the other end portion, and a hollow portion formed to have a predetermined length and open at the other end portion;a branch pipe which is connected to a side wall of the first rod and communicates with the hollow portion;a second rod having one end portion connected to the push-pull rod, the other end portion, and a recess portion formed in a part of a side wall of a portion which extends a predetermined length from the other end portion to the one end portion side and is inserted in the hollow portion; andan engaging member arranged to be freely movable in the branch pipe, which is engagable with the recess portion.

REFERENCES:
patent: 5042749 (1991-08-01), Jacques et al.
patent: 5823471 (1998-10-01), Dazet
Murayama, Daijiro, “Aeronautical Engineering Course,” autopilot, Apr. 10, 1983, vol. 17, Japan Aeronautical Engineer's Association, Japan.

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